EP3339017B1 - Method for manufacturing a weldable metal-polymer multilayer composite - Google Patents

Method for manufacturing a weldable metal-polymer multilayer composite Download PDF

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Publication number
EP3339017B1
EP3339017B1 EP16206337.4A EP16206337A EP3339017B1 EP 3339017 B1 EP3339017 B1 EP 3339017B1 EP 16206337 A EP16206337 A EP 16206337A EP 3339017 B1 EP3339017 B1 EP 3339017B1
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EP
European Patent Office
Prior art keywords
metallic
metal
metal layers
layers
sandwich
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EP16206337.4A
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German (de)
English (en)
French (fr)
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EP3339017A1 (en
Inventor
Philip Ninnemann
Thomas HÜNDGEN
Thomas Fröhlich
Stefan Lindner
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Outokumpu Oyj
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Outokumpu Oyj
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Priority to EP16206337.4A priority Critical patent/EP3339017B1/en
Application filed by Outokumpu Oyj filed Critical Outokumpu Oyj
Priority to PL16206337T priority patent/PL3339017T3/pl
Priority to ES16206337T priority patent/ES2845692T3/es
Priority to CA3047640A priority patent/CA3047640A1/en
Priority to JP2019534369A priority patent/JP6865284B2/ja
Priority to AU2017380882A priority patent/AU2017380882B2/en
Priority to US16/472,343 priority patent/US12115592B2/en
Priority to MX2019007147A priority patent/MX2019007147A/es
Priority to KR1020197019542A priority patent/KR102489869B1/ko
Priority to CN201780078981.3A priority patent/CN110087874B/zh
Priority to BR112019012575-2A priority patent/BR112019012575B1/pt
Priority to RU2019118778A priority patent/RU2753692C2/ru
Priority to MYPI2019003534A priority patent/MY193290A/en
Priority to PCT/EP2017/082855 priority patent/WO2018114606A1/en
Priority to TW106144863A priority patent/TWI758381B/zh
Publication of EP3339017A1 publication Critical patent/EP3339017A1/en
Priority to ZA2019/04060A priority patent/ZA201904060B/en
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Publication of EP3339017B1 publication Critical patent/EP3339017B1/en
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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K11/00—Resistance welding; Severing by resistance heating
    • B23K11/06—Resistance welding; Severing by resistance heating using roller electrodes
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B37/00—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
    • B32B37/06—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the heating method
    • B32B37/065—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the heating method resulting in the laminate being partially bonded
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K11/00—Resistance welding; Severing by resistance heating
    • B23K11/002—Resistance welding; Severing by resistance heating specially adapted for particular articles or work
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K11/00—Resistance welding; Severing by resistance heating
    • B23K11/10—Spot welding; Stitch welding
    • B23K11/11—Spot welding
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K11/00—Resistance welding; Severing by resistance heating
    • B23K11/16—Resistance welding; Severing by resistance heating taking account of the properties of the material to be welded
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B15/00—Layered products comprising a layer of metal
    • B32B15/04—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material
    • B32B15/043—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material of metal
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B15/00—Layered products comprising a layer of metal
    • B32B15/04—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material
    • B32B15/08—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material of synthetic resin
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B15/00—Layered products comprising a layer of metal
    • B32B15/04—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material
    • B32B15/08—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material of synthetic resin
    • B32B15/092—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material of synthetic resin comprising epoxy resins
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B15/00—Layered products comprising a layer of metal
    • B32B15/18—Layered products comprising a layer of metal comprising iron or steel
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B15/00—Layered products comprising a layer of metal
    • B32B15/20—Layered products comprising a layer of metal comprising aluminium or copper
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B27/00—Layered products comprising a layer of synthetic resin
    • B32B27/38—Layered products comprising a layer of synthetic resin comprising epoxy resins
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B3/00—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form
    • B32B3/26—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a particular shape of the outline of the cross-section of a continuous layer; characterised by a layer with cavities or internal voids ; characterised by an apertured layer
    • B32B3/28—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a particular shape of the outline of the cross-section of a continuous layer; characterised by a layer with cavities or internal voids ; characterised by an apertured layer characterised by a layer comprising a deformed thin sheet, i.e. the layer having its entire thickness deformed out of the plane, e.g. corrugated, crumpled
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B7/00—Layered products characterised by the relation between layers; Layered products characterised by the relative orientation of features between layers, or by the relative values of a measurable parameter between layers, i.e. products comprising layers having different physical, chemical or physicochemical properties; Layered products characterised by the interconnection of layers
    • B32B7/04—Interconnection of layers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B7/00—Layered products characterised by the relation between layers; Layered products characterised by the relative orientation of features between layers, or by the relative values of a measurable parameter between layers, i.e. products comprising layers having different physical, chemical or physicochemical properties; Layered products characterised by the interconnection of layers
    • B32B7/04—Interconnection of layers
    • B32B7/05—Interconnection of layers the layers not being connected over the whole surface, e.g. discontinuous connection or patterned connection
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B7/00—Layered products characterised by the relation between layers; Layered products characterised by the relative orientation of features between layers, or by the relative values of a measurable parameter between layers, i.e. products comprising layers having different physical, chemical or physicochemical properties; Layered products characterised by the interconnection of layers
    • B32B7/04—Interconnection of layers
    • B32B7/12—Interconnection of layers using interposed adhesives or interposed materials with bonding properties
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K2103/00—Materials to be soldered, welded or cut
    • B23K2103/02—Iron or ferrous alloys
    • B23K2103/04—Steel or steel alloys
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K2103/00—Materials to be soldered, welded or cut
    • B23K2103/02—Iron or ferrous alloys
    • B23K2103/04—Steel or steel alloys
    • B23K2103/05—Stainless steel
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K2103/00—Materials to be soldered, welded or cut
    • B23K2103/08—Non-ferrous metals or alloys
    • B23K2103/10—Aluminium or alloys thereof
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K2103/00—Materials to be soldered, welded or cut
    • B23K2103/08—Non-ferrous metals or alloys
    • B23K2103/15—Magnesium or alloys thereof
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K2103/00—Materials to be soldered, welded or cut
    • B23K2103/16—Composite materials, e.g. fibre reinforced
    • B23K2103/166—Multilayered materials
    • B23K2103/172—Multilayered materials wherein at least one of the layers is non-metallic
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K2103/00—Materials to be soldered, welded or cut
    • B23K2103/18—Dissimilar materials
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2250/00—Layers arrangement
    • B32B2250/04—4 layers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2250/00—Layers arrangement
    • B32B2250/40—Symmetrical or sandwich layers, e.g. ABA, ABCBA, ABCCBA
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2307/00—Properties of the layers or laminate
    • B32B2307/20—Properties of the layers or laminate having particular electrical or magnetic properties, e.g. piezoelectric
    • B32B2307/202—Conductive
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2419/00—Buildings or parts thereof
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2605/00—Vehicles
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2605/00—Vehicles
    • B32B2605/08—Cars
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2605/00—Vehicles
    • B32B2605/10—Trains

Definitions

  • the present invention relates to a method for manufacturing a weldable metal-polymer multilayer composite as a semi-finished product where a resistance heating process is used to have a substance to substance bond between the different metal layers and to have therefore at the end a continuous material resistance for the whole composite. Then during a subsequent component manufacturing step the composite is dissimilar weldable to other metal components, sheets or composites. The subsequent processing industry can then directly use the semi-finished multilayer composite for further resistance welding processes.
  • Composite structures can be fabricated from a wide variety of metallic, polymeric, ceramic or organic materials in different structures and combinations. Stamm K., Witte H., Sandwichkonstruktionen. Springer-Verlag, Wien, New York, 1974 shows different design variations for such composite constructions. According to the literature, composite structures can be differentiated between infiltrated composites, corpuscles compounds, fiber composites or multilayer composites. Layer composites are macroscopically inhomogeneous. One kind of a layer composite is sandwich constructions defined as structures having several layers with respectively specific material properties. One further characteristic is that the different layers are flat ordered and parallel orientated to each other. A typical upset of a sandwich structure is two metallic outer-layers bonded to a polymer core material from two sides. The core layers can be further differentiated with regard to their supporting effect: Core materials having a support effect
  • sandwich designs are a high lightweight potential with at the same time a high stiffness and strength level.
  • the design of a sandwich can be component-dependent adjusted to the level and directions of the component loads. Additionally significant higher mechanical as well as acoustic energy absorption can be realised in comparison to monolithic materials. Aerospace as well as automotive engineering, engineering of commercial vehicles, motorcycles, agricultural as well as railway vehicles, ship and building constructions, containers or the industry of renewables energies are only some processing industries using the mentioned advantages of sandwich structures.
  • the thermal energy is at this point the highest, too.
  • the thermal energy at this point reaches the melting temperature of the sheets and a weld point or called weld nugget results.
  • the effect can be reached at different transition points of the materials, depending on the physical properties of the used metallic materials. Thereby the effect can be occurring wanted (like a three sheet combination in automotive car body engineering) or unwanted, e.g. when a metallic contact is undesired created for origin isolated electric engineering components.
  • R G R M + R T wherein R M is the sum of all material resistances and R T is the sum of all transition resistances.
  • R M ⁇ EL * L / A wherein ⁇ EL is the specific electrical resistance of the material, L is the conductor length and A as the conductor cross section.
  • Typical sandwich panels with a flat order of the different layers are mentioned in the WO publications 2014009114A1 , 2014001152A9 , 2012048844A1 , and 2013156167A1 as well as in the Tata steel data sheet "Coretinium® - A unique and durable composite solution that delivers light-weight products and design innovation" (Internet address: http://www.tatasteeleurope.com/static_files/Downloads/Construction/Coretinium /Coretinium%20gen%20app%20data%20sheet.pdf).
  • WO publications 2008125228A1 and 2004002646A1 describe a method for manufacturing a metallic sandwich structure wherein the different layers are bonded together. All these WO publications have the same disadvantage of having an isolating material between the metallic outer-layers which results in a non-resistance-weldability.
  • the JP publication H01-127125 describes a method for manufacturing a sandwich panel containing two sheet metal layers and one corrugated element. Spot welding is used to fit the first sheet metal layer to one surface of a corrugated strip. Then a bonding tape process follows. A pair of press roller machines is used to fit the second sheet metal layer to the second surface of the corrugated strip by pressurizing and bonding.
  • the disadvantage of the resulting semi-finished product is the fact that the subsequent processing industry like car body manufacturer cannot use these kinds of sandwich products for further resistance welding processes to join this sandwich panel with other car body sheets, plates or formed components together. The reason is that the mentioned bonding tape works as an isolator for the electric circuit in a resistance welding process. No weld nugget and therefore no connection can be created.
  • the JP patent publication H02-78541A describes a method how to produce a sandwich structure wherein recessed parts are produced on the outside surface of one metal sheet in a laminate formed by interposing resin. It is worked out that the distance between the tip of the projected part and the inside surface of the other metal sheet are specified with the distance. That means, in spite of using a profiled outer-layer steel sheet, there will be at the end a defined isolating gap between both metal sheets which results in a non-resistance weldable configuration.
  • the EP patent publication 1059160A2 describes a composite material wherein the core layer is firmly attached with two outer-layers. But the layer materials are characterized as non-metallic (textile patterns) and the contact is not material closured. Notwithstanding that this EP publication is the first quoted one, which describes a continuous contact over the whole composite thickness, and resistance weldability is therefore non-existent.
  • WO patent publication 03082573A1 and the US patent publication 2005126676A1 describe devices and methods for the production of composite materials.
  • the core layer contains also metallic elements in kind of short-cut fibers. But a continuous material closure over the complete height of the sandwich structure is not possible because on both outer-layers an adhesive is applied during the first manufacturing steps.
  • Related design variations are also known from EP patent publication 1059160A2 , where non-weldable spacer textiles are used for the core material, or WO patent publication 9801295A1 and EP patent publication 0333685A2 , where fibers as a core material are applied by electrostatic precipitation or rather electrostatic deposition.
  • the WO patent publication 2016097186A1 describes a way how to manufacture a sandwich panel as a semi-finished product where at least one three dimensional metallic layer is used to achieve a directly mechanical contact between all metallic layers and therefore to enable a current flow during resistance welding because of the therefore closed electric circuit.
  • One disadvantage of this publication for joining this sandwich panel to other metallic sheets or components is that there is not a material closure of all metallic layers, only a directly mechanical contact which works during spot welding as a further transition resistance additionally to the original transition resistance between the sandwich panel and another metallic sheet or component. Therefore it is possible that the weld nugget results in the transition zones of the different sandwich layers and not in the transition zone of the sandwich panel and the other sheet, depending on the material combination, material thicknesses and physical properties like heat conduction or thermal capacity of the materials.
  • a first composite sheet metal part comprising at least two metal sheets and a sheet arranged between both metal sheets that consists of a material with a different composition than the two metal sheets, is welded to a second sheet metal part consisting of a solid metallic material or a further composite material with at least two metal sheets and a sheet arranged between the metal sheets that consists of a material with a different composition than the two metal sheets.
  • a method how to weld sandwich panels with resistance spot welding is mentioned in the WO publication 2011082128A1 , wherein the composite core material of a sandwich panel is layered by two metallic outer-layers.
  • the target of creating specific resistance weldability is solved by having a plurality of steel fibers in the core-layer which arrange the electrical communication with the outer-layer steel sheets.
  • One disadvantage is the reproducibility and repeatability of welding results. There is no guarantee to have the right and sufficient numbers of steel fibres in contact when a subsequent manufacturer wants to use the welding parameters. There is a big danger to create weld spatters in the contact areas of the steel-fibre with the steel outer-layers and to burn the non-metallic parts around it. Additional to the softening and displacing of the non-metallic interlayer, also and described in detail in the following publications, is mentioned as one way to solve the target.
  • the same additional process steps are worked out by the DE publication 102011109708A1 , which describes also a subsequent process to make a sandwich structure weldable where the both metallic outer-layers are not in directly contact in the initial state.
  • the FR publication 2709083A1 describes a typical sandwich panel with two metallic outer-layer sheets and a non-metallic core material which isolates the two outer-layers.
  • the same approach like in the DE publication 102011054362A1 is used: to soften and displace the non-metallic core material at the border area of the sheets.
  • the WO patent publication 2014121940A1 A describes a further way to join a sandwich.
  • the sandwich panel is defined as a structure with two metal faces and an insulating core material. That definition results in a non-weldability in the initial state of the sandwich.
  • a joint, not with resistance welding, is only possible after a further production step to achieve a tongue portion at a first side face and a groove portion at an opposite second side face of the panel, wherein the tongue portion and the groove portion of adjoining panels engage each other on the assembly to form a joint between the adjoining panels.
  • the object of the present invention is to prevent the drawbacks of the prior art and to achieve an improved method for manufacturing a semi-finished sandwich panel wherein a continuous metallic material closure is ensured for subsequent resistance welding processes.
  • a continuous metallic material closure is ensured for subsequent resistance welding processes.
  • the non-hardened and non-metallic material is repressed from the metallic contacts and the different metal layers are welded together as a so-called tack welding.
  • the essential features of the present invention are enlisted in appended claim1.
  • At least two metal layers wherein at least one metal layer is applied by using a three dimensional metal sheet is combined with at least one non-metallic layer in a non-cured and non-hardened state between the metal layers.
  • a resistance welding process is carried out in order to achieve a tack welding, which means that there is a complete metallic contact resulting in a continuous metallic material closure over the whole sandwich structure.
  • a sandwich panel is manufactured from at least two metal layers and at least one non-metallic and non-hardened layer positioned in the recess spaces formed between two metal layers when at least one of the metal layers is shaped being a corrugated metal strip as a three dimensional object.
  • the non-metallic and non-hardened layer is filled completely into the recess spaces formed between two metal layers.
  • a preferably temperature for an epoxy resin is between 35 and 65 °C, preferably between 40 and 65 °C to reach a viscosity over 500 mPas.
  • the corrugated metal strip can be optionally heated to at most 80 °C, preferably also between 55 and 65 °C to increase the flow behaviour of the filled-in non-metallic material.
  • the electrode force is important to repress the non-hardened non-metallic material from the metallic contacts of the different metal layers but not to destroy the structure as well as the particular layer of the sandwich, such as distortion. Therefore, ; an electrode force of 1,0 kN - 3,0 kN, preferably 1,8 kN - 2,5 kN is used. Then the electrode force enables a metallic contact for the weld on the one side, but also persists a high filling degree of the non-metallic non-hardened layer on the other side with adhesion contacts to all metallic layers.
  • the advantage of the tack weld, utilized according to the invention, is that the non-metallic material is not damaged because of the high welding current or liquid metal during welding. Further, the tack weld enables subsequent forming operations, e.g. a deep-drawing process to create a formed component out of the flat sandwich sheet. A tack weld creates an advantageous stiffness of the sandwich like a normal weld. On the other side the tack weld enables a good handling stability during manufacturing of the sandwich structure before the adhesive is hardened.
  • the joint of the layers caused by the combination of the tack weld on the one side and the bond of the adhesive on the other side, enables a high form stability without a delamination of the different layers during different cutting or stamping technologies like laser cutting, water jet cutting, plasma cutting or mechanical cutting.
  • the layer adhesion of the present invention is worked out favourable embodiment when the adhesion of the tack weld is lower than the adhesion of the non-metallic adhesive. As a result bending angles over 130 degrees without any delamination of the layers can be reached.
  • the resistance roller seam method is a cost-efficient manufacturing process which is further easy to automatable with a high welding speed more than 4m/min.
  • tack welding in accordance with the present invention, to use a sandwich structure in initial, delivery state directly for a following resistance welding process, i. e. the sandwich structure is achieved to create a closure electrical circuit as well as to steer the resulting weld to the contact area of the sandwich structure with another metal component
  • a metal layer 1 and a three dimensional metal layer 2 are tack welded 3 to each other.
  • a recess space 4 between the metal layers 1 and 2 is filled with a polymer material.
  • a third metal layer 5 is shown also a third metal layer 5.
  • the metal layer 5 is tack welded 8 with the metal layer 2.
  • a recess space 6 between the metal layers 2 and 5 is filled with a polymer material.
  • Fig. 1 shows an example of the amplitude 7 between two tack welds 8.
  • Fig. 2 shows a solution for the sandwich structure of Fig. 1 where the sandwich structure is spot welded 11 with an external component 12.
  • a non-metallic adhesion layer is used for the non-metallic core as a contrast to most state of the art sandwich structures where a sandwich panel is build up with two metallic outer layers and with two layers of adhesion to bond both outer layers with the middle positioned core material. Therefore, the sandwich structure of the present invention can be created with a more simple manufacturing line and with increased clock frequency. The sandwich structure is cheaper because of saving two layers compared to the state of the art sandwich panels.
  • the recurring metal contacts have an amplitude lower than 5.0 mm, whereby a welding current for each amplitude of 1.0 - 1.4 kA is used to create the tack weld.
  • the form of the three dimensional layer in combination with the chosen non-metallic material and the filling degree of the non-metallic material in the recess spaces formed between the metal layers, gives for these panels their mechanical, stiffness, sound, joining and process features.
  • the first and second metal layers in the manufacture of a sandwich panel according to the invention are advantageously made of the same material, such as stainless steel, carbon steel, copper, aluminium, magnesium, but the first and second metal layers can also be made of different metal materials, different metals or different metal compositions. However, when using different metals or different metal compositions the combination of these metals can further alter the behaviour of the sandwich panel. For instance, a combination of metals with different thermal expansion coefficients can be advantageous in some solutions of the present invention. By using two metals with two different thermal expansion coefficients can influence the thermal expansion of the sandwich panel, and the surface of the three-dimensional sheet will avoid disruption in the welded areas of the sandwich panel.
  • the sandwich panel of the present invention with two different metal layers can be used as a component bridge in wet-corrosion areas of multi-material designed car bodies.
  • a foot of a b-pillar is manufactured with stainless steel and a rocker rail is manufactured with aluminium
  • the sandwich panel can be used as a connection between the two parts.
  • the aluminium side of the sandwich is welded to the aluminium rocker rail and the stainless sandwich layer is welded with the stainless b-pillar.
  • the only potential bridge is then in the sandwich, but the non-metallic layer isolates big areas and the residual metallic contact are small (linear or point contact) in comparison to the component size.
  • the three dimensional metal layer in the manufactured sandwich panel of the invention is a corrugated metal piece which is mechanically connectable with the essentially flat two-dimensional first metal layer.
  • Suitable shapes for the second metal layer are found for instance in the WO publication 2014/096180 .
  • the form of the second metal layer also determines damping, noise, vibration, stiffness, especially the buckling stiffness, and weldability of the sandwich panel.
  • Nubs and knobs profiled sheets result in a direction independent stiffness but are only suitable weldable with resistance spot welding because of the punctual contact.
  • Corrugated profiled sheets have a direction depending stiffness but enable welding with all continuous welding procedures like resistance roller seam welding because of the linear contact.
  • the second metal layer can have a shape of an essentially sinusoidal wave, or the second layer can have a shape of a corrugated strip where the two parts of the strip next to each other are in the essentially perpendicular position to each other. Also other shapes of a corrugated strip can be used for the second layer in the sandwich panel manufactured according to the invention.
  • the non-metallic layer between the two metal layers in the sandwich panel of the invention is advantageously made of polymer material, resin material, sealant material, cold or thermosetting one or two component adhesive glues, for instance a crash-resistant one component adhesion glue used in the automotive industry or a two component sandwich-adhesion material containing resin and hardener.
  • the essential properties of the non-metallic interlayer are non-cured and non-hardened condition during set-up of the sandwich and the viscosity during applying and the way of curing and foaming.
  • a good viscosity to reach a defined filling degree without destroying the metallic contact areas is between 400 and 10000 mPas, more preferably greater than 500 mPas.
  • a more advantageous embodiment of the non-metallic layer has viscoplastic or thixotropic properties and a specific weight of 1.0 - 1.1 g/cm 3 .
  • a preheating of the non-metallic material before applying can be suitable to reach the right applying viscosity, depending on the chosen polymer and preferred at the temperature range between 40 and 65 °C.
  • the different metal layers in the sandwich panel of the invention are attached to each other by the combination of bonding to the adhesive and the metallic material closure resistance weld so that a subsequent resistance welding, in order to connect the semi-finished product to a construction of a desired combination of solutions, to other sheets, plates or formed parts will be focused on the points where the first metal layer and the second metal layer has a metallic material closure to each other.
  • the distance ⁇ between the different material closure contacts inside the sandwich should be so small that in every case of the later position to other components, an electric circuit is enabled to build as a result the weld nugget between the other component and one of the outer layers of the sandwich structure.
  • a suitable distance for the invention is ⁇ ⁇ 5.5 mm, preferably ⁇ ⁇ 2.5 mm.
  • the sandwich structure of the present invention is used in a subsequent manufacturing process like car body engineering of passenger cars, commercial, agricultural or railway vehicles, especially in wet-area parts or parts like the car roof, cowl/front wall, channel, inlayer of a pillar, front lid or in noise relevant applications like container.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Laminated Bodies (AREA)
  • Resistance Welding (AREA)
  • Lining Or Joining Of Plastics Or The Like (AREA)
EP16206337.4A 2016-12-22 2016-12-22 Method for manufacturing a weldable metal-polymer multilayer composite Active EP3339017B1 (en)

Priority Applications (16)

Application Number Priority Date Filing Date Title
PL16206337T PL3339017T3 (pl) 2016-12-22 2016-12-22 Sposób wytwarzania zgrzewalnego wielowarstwowego kompozytu metal-polimer
ES16206337T ES2845692T3 (es) 2016-12-22 2016-12-22 Método de fabricación de un compuesto multicapa de metal-polímero soldable
EP16206337.4A EP3339017B1 (en) 2016-12-22 2016-12-22 Method for manufacturing a weldable metal-polymer multilayer composite
MYPI2019003534A MY193290A (en) 2016-12-22 2017-12-14 Method for manufacturing a weldable metal-polymer multilayer composite
AU2017380882A AU2017380882B2 (en) 2016-12-22 2017-12-14 Method for manufacturing a weldable metal-polymer multilayer composite
US16/472,343 US12115592B2 (en) 2016-12-22 2017-12-14 Method for manufacturing a weldable metal-polymer multilayer composite
MX2019007147A MX2019007147A (es) 2016-12-22 2017-12-14 Procedimiento de fabricacion de un compuesto multicapa de metal-polimero soldable.
KR1020197019542A KR102489869B1 (ko) 2016-12-22 2017-12-14 용접가능한 금속-중합체 다층 복합물을 제조하는 방법
CA3047640A CA3047640A1 (en) 2016-12-22 2017-12-14 Method for manufacturing a weldable metal-polymer multilayer composite
BR112019012575-2A BR112019012575B1 (pt) 2016-12-22 2017-12-14 Método para fabricar um painel em sanduíche como um produto semiacabado
RU2019118778A RU2753692C2 (ru) 2016-12-22 2017-12-14 Способ изготовления пригодного для сварки многослойного композита металл-полимер
JP2019534369A JP6865284B2 (ja) 2016-12-22 2017-12-14 溶接可能な金属−ポリマ複層複合材料の製造方法
PCT/EP2017/082855 WO2018114606A1 (en) 2016-12-22 2017-12-14 Method for manufacturing a weldable metal-polymer multilayer composite
CN201780078981.3A CN110087874B (zh) 2016-12-22 2017-12-14 用于制造可焊接金属-聚合物多层复合材料的方法
TW106144863A TWI758381B (zh) 2016-12-22 2017-12-20 可焊金屬-聚合物多層複合材料之製造方法
ZA2019/04060A ZA201904060B (en) 2016-12-22 2019-06-21 Method for manufacturing a weldable metal-polymer multilayer composite

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EP (1) EP3339017B1 (ru)
JP (1) JP6865284B2 (ru)
KR (1) KR102489869B1 (ru)
CN (1) CN110087874B (ru)
AU (1) AU2017380882B2 (ru)
BR (1) BR112019012575B1 (ru)
CA (1) CA3047640A1 (ru)
ES (1) ES2845692T3 (ru)
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MY (1) MY193290A (ru)
PL (1) PL3339017T3 (ru)
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KR102489869B1 (ko) 2023-01-17
WO2018114606A1 (en) 2018-06-28
TW201829107A (zh) 2018-08-16
AU2017380882B2 (en) 2023-05-25
TWI758381B (zh) 2022-03-21
BR112019012575A2 (pt) 2019-11-19
CN110087874B (zh) 2021-05-18
BR112019012575B1 (pt) 2023-01-31
RU2019118778A3 (ru) 2021-03-11
CA3047640A1 (en) 2018-06-28
ES2845692T3 (es) 2021-07-27
US20190358731A1 (en) 2019-11-28
EP3339017A1 (en) 2018-06-27
US12115592B2 (en) 2024-10-15
PL3339017T3 (pl) 2021-06-14
ZA201904060B (en) 2021-10-27
RU2753692C2 (ru) 2021-08-19
JP2020514112A (ja) 2020-05-21
MX2019007147A (es) 2019-08-16
JP6865284B2 (ja) 2021-04-28
CN110087874A (zh) 2019-08-02
MY193290A (en) 2022-10-01
AU2017380882A1 (en) 2019-07-04
KR20190090853A (ko) 2019-08-02
RU2019118778A (ru) 2021-01-22

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